DocumentCode
3264533
Title
Design and integration of a solar AMTEC power system with an advanced global positioning satellite
Author
Johnson, G. ; Hunt, M.E. ; Determan, W.R. ; HoSang, P.A. ; Ivanenok, J. ; Schuller, M.
Author_Institution
Rocketdyne Div., Rockwell Int. Corp., Canoga Park, CA, USA
Volume
1
fYear
1996
fDate
11-16 Aug 1996
Firstpage
623
Abstract
A 1,200 W solar AMTEC (alkali metal thermal-to-electric conversion) power system concept was developed and integrated with an advanced global positioning system (GPS) satellite. The critical integration issues for the SAMTEC with the GPS subsystems included: (1) packaging within the Delta II launch vehicle envelope; (2) deployment and start-up operations for the SAMTEC; (3) SAMTEC operation during all mission phases; (4) satellite field of view restrictions with satellite operations; and (5) effect of the SAMTEC requirements on other satellite subsystems. The SAMTEC power system was compared with a conventional planar solar array/battery power system to assess the differences in system weight, size and operations. Features of the design include the use of an advanced multitube, vapor anode AMTEC cell design with 24% conversion efficiency, and a direct solar insolation receiver design with integral LiF salt canisters for energy storage to generate power during the maximum solar eclipse cycle. The modular generator design consists of an array of multitube AMTEC cells arranged into a parallel/series electrical network with built-in cell redundancy. Their preliminary assessment indicates that the solar generator design is scaleable over a 500 to 2,500-W range. No battery power is required during the operational phase of the GPS mission. SAMTEC specific power levels greater than 5 We/kg and 160 We/m2 are anticipated for a mission duration of 10 to 12 yr in orbits with high natural radiation backgrounds
Keywords
Global Positioning System; artificial satellites; solar absorber-convertors; space vehicle power plants; thermoelectric conversion; 10 to 12 y; 1200 W; 24 percent; 500 to 2500 W; Delta II launch vehicle; GPS; deployment; design; direct solar insolation receiver; global positioning satellite; satellite subsystems; solar AMTEC power system; space power; start-up; Anodes; Batteries; Energy storage; Global Positioning System; Packaging; Power generation; Power systems; Satellites; Solar power generation; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety
Conference_Location
Washington, DC
ISSN
1089-3547
Print_ISBN
0-7803-3547-3
Type
conf
DOI
10.1109/IECEC.1996.552965
Filename
552965
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